View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 12792U 26074.51932235 +.00000000 +00000-0 +56376-4 0 00004
2 12792 74.0271 272.9354 0012989 146.6945 213.5029 14.39011230 06
| Epoch (UTC): | 15 March 2026 12:27:49 |
| Eccentricity: | 0.0012989 |
| inclination: | 74.0271° |
| perigee height: | 752 km |
| apogee height: | 771 km |
| right ascension of ascending node: | 272.9354° |
| argument of perigee: | 146.6945° |
| revolutions per day: | 14.39011230 |
| mean anomaly at epoch: | 213.5029° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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